View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 13341.85290821 .00000012 00000-0 45692-4 0 2586
2 24278 098.5320 016.9865 0351471 074.0905 027.7930 13.53010981854795
| Epoch (UTC): | 07 December 2013 20:28:11 |
| Eccentricity: | 0.0351471 |
| inclination: | 98.5320° |
| perigee height: | 800 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 16.9865° |
| argument of perigee: | 74.0905° |
| revolutions per day: | 13.53010981 |
| mean anomaly at epoch: | 27.7930° |
| orbit number at epoch: | 85479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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